▸Orbital parameters

Orbit class	LEO
Inclination	49.9926°
Eccentricity	0.0017923
Period	97.0 min
Apogee	629 km
Perigee	604 km
Mean motion	14.84102763 rev/day
RAAN	81.7374°
Arg of perigee	129.8930°
Mean anomaly	230.3587°
B*	2.2578e-4
Rev at epoch	4,939

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 65125U 25170G 26188.12976500 .00001678 00000-0 22578-3 0 9998

2 65125 49.9926 81.7374 0017923 129.8930 230.3587 14.84102763 49393

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 07",
  "OBJECT_ID": "2025-170G",
  "EPOCH": "2026-07-07T03:06:51.696+00:00",
  "MEAN_MOTION": 14.84102763,
  "ECCENTRICITY": 0.0017923,
  "INCLINATION": 49.9926,
  "RA_OF_ASC_NODE": 81.7374,
  "ARG_OF_PERICENTER": 129.893,
  "MEAN_ANOMALY": 230.3587,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65125,
  "REV_AT_EPOCH": 4939,
  "BSTAR": 0.00022578,
  "MEAN_MOTION_DOT": 0.00001678,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	GEESAT-4 07
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Aug 8, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	130HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/65125

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.